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AD 75-26-17 ACTIVE

Engine Mount
Key Information
AD Number 75-26-17 Status Active
Effective Date January 17, 1976 Issue Date Not specified
Docket Number Unknown Amendment 39-2466
Product Type ["Aircraft"] Product Subtype ["Small Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Pilatus Aircraft Limited
Model(s) PC-6/A
Regulatory Text

75-26-17 PILATUS AIRCRAFT LTD: Amendment 39-2466. Applies to Pilatus Model PC-6/A airplanes up to and including S/N 659 (all variants) with Astazou engine installations manufactured by Pilatus Aircraft Ltd.
NOTE: This AD does not apply to Pilatus Model PC-6/A airplanes manufactured by Fairchild Hiller.
Compliance required within the next 100 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent failure of the engine mount to fuselage attachment, reinforce the U-channel, P/N 6201.992, by installing a steel plate, P/N 112.35.06.337, to each U-channel lug and rework the engine strut heads, P/N 6501.106, in accordance with paragraph 2.2 of Pilatus Aircraft Ltd. Service Bulletin No. 83A dated February 1971, or an FAA-approved equivalent.
This amendment becomes effective on January 17, 1976.